SATPC0039973 Tab 04 Drawing 5 (FLL-HPROJ-0011_-).pdf

7 6 5 4 3

B B

C C

7 6 5 4 2

2 1

A

8 3

D

A

D

NOTES - UNLESS OTHERWISE SPECIFIED:

48X .812 +.010 -.001

THRU

4X R1.000

1.00

X

X

X

X

X

X

X

X

X

X

X

X

135.820

23.937

12X 7.062

12X .000

12X 14.124

12X 21.186

22.561

9.000

8.000

4X 7.516

REVISION HISTORY

CHECKENGRDATEDESCRIPTIONREV

2025-09-23APPROVED FOR INITIAL RELEASE -

SHEET 1 OF 9CI NO. SCALE: 0.125

-FLL-HPROJ-00111JYR2D

REV.DWG. NO.CAGESIZE

STRONGBACK PLATES

TITLE

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

ARMSTRONG FLIGHT RESEARCH CENTER

EDWARDS, CALIFORNIA

2025-04-22A.C. HOLGUINENGR

2025-09-23C.A. MASELLACHECK

REVIEW

2025-09-23L.D. HUDSONREVIEW

2025-04-22A.C. HOLGUINDRAWN

2025-04-22A.C. HOLGUINDESIGN

DATEAPPROVALS

THIRD ANGLE PROJECTION

DO NOT SCALE DRAWING

DECIMALS

.X .1

.XX .03

.XXX .010

.XXXX .0010

ANGLES

.X 0.5

.XX 0.25

UNLESS OTHERWISE SPECIFIED DIMENSIONS

ARE IN INCHES. TOLERANCES ARE:

PARTS SHALL BE FREE OF

BURRS AND SHARP EDGES

INTERPRET DRAWING PER

ASME Y14.100

USED ONNEXT ASSEMBLY

FLLFLL-HPROJ-0003

PARTS LIST

NOTES

MATERIAL

SPECIFICATION

NOMENCLATURE

OR DESCRIPTION

PART OR

IDENTIFYING NO.

CAGE CODE

ITEM

NO.QTY REQD

.062 A

1 MAKE FROM PART NUMBER <part number>, CAGE CODE <cagecode>

2 SURFACE ROUGHNESS ON MACHINED SURFACES SHALL BE 125

MICROINCHES MAX

3 DRILL POINT ACCEPTABLE PAST INDICATED DEPTH

4 STOCK RADII ACCEPTABLE

5 WELD PER AMERICAN WELDING SOCIETY SPECFICITION AWS

D17.1/D17.1M, GROUP <from below>, CLASS <from below>

Groups:

IA= Carbon & alloy steels IB= Heat treatable alloy steels

IIA= CRES

IIB= Precip hardening CRES IV= Alum alloys

Classes:

A= Critical B= Medium C= Non-critial

6 WELD PER AMERICAN WELDING SOCIETY SPECIFICATION AWS

D1.1/D1.1M USING <welding process> WITH <filler metal>.

<inspection requirements>

7 HEAT TREAT PER SOCIETY OF AUTOMOTIVE ENGINEERS (SAE)

SPECIFICATION AMS2759, ROCKWELL C HARDNESS <min hardness> TO <max hardness>

8 HEAT TREAT PER SOCIETY OF AUTOMOTIVE ENGINEERS (SAE)

SPECIFICATION AMS2770 TO <T##> TEMPER

9 PASSIVATE PER ASTM A967/A967M USING NITRIC 4 SOLUTION

10 CHEMICAL CONVERSION (ALODINE) FINISH PER MIL-DTL-5541,

CLASS <from below>

Classes:

1A= Max protection from corrosion 3= Low electrical resistance

11 ANODIZE PER MIL-A-8625, TYPE II, CLASS <1=no dye, 2=dye>, DYE <color> BEFORE SEALING. PLUG ALL THREADED

HOLES

12 CADMIUM PLATE PER SOCIETY OF AUTOMOTIVE ENGINEERS

(SAE) SPECIFICATION AMS-QQ-P-416, TYPE <I=As plated, II=chromate, III=phosphate>, CLASS <1=.0005" Thick, 2=.0003" Thick, 3=.0002" Thick>

13 POWDER COAT FINISH AS FOLLOWS:

A. CHEMICAL CONVERSION (ALODINE) FINISH PER MIL-DTL-

5541, CLASS 1A.

B. POWDER COAT AND OVEN CURE PER MANUFACTURER'S

INSTRUCTIONS. COLOR <color number from below> (<color name>) PER SOCIETY OF AUTOMOTIVE ENGINEERS

(SAE) SPECIFICATION AMS-STD-595

14 PRIMER/TOP COAT FINISH PER MIL-DTL-18264 AS FOLLOWS:

A. CHEMICAL CONVERSION (ALODINE) FINISH PER MIL-DTL-

5541, CLASS 1A

B. ONE COAT MIL-PRF-23377 EPOXY PRIMER, TYPE I, CLASS

<C1, C2, or N> C. TWO COATS MIL-PRF-85285 POLYURETHANE, TYPE <type>, COLOR <color number from below> (<color name>) PER

SOCIETY OF AUTOMOTIVE ENGINEERS (SAE)

SPECIFICATION AMS-STD-595

15 PRIMER ONLY FINISH PER MIL-DTL-18264 AS FOLLOWS:

A. CHEMICAL CONVERSION (ALODINE) FINISH PER MIL-DTL-

5541, CLASS 1A

B. TWO COATS MIL-DTL-23377 YELLOW EPOXY PRIMER, TYPE

I, CLASS <C1, C2, or N>

11136 (GLOSS INSIGNIA RED)

12197 (GLOSS INTERNATIONAL ORANGE)

13538 (GLOSS HIGHWAY YELLOW)

15044 (GLOSS INSIGNIA BLUE)

15050 (GLOSS POST OFFICE BLUE)

17038 (GLOSS BLACK)

16473 (GLOSS NASA AIRCRAFT GRAY)

17925 (GLOSS WHITE)

36118 (FLAT GUNSHIP GRAY)

36173 (FLAT OCEAN GRAY)

36176 (FLAT OCEAN GRAY)

36251 (FLAT GRAY)

36270 (FLAT HAZE GRAY)

37038 (FLAT BLACK)

SHERWIN WILLIAMS P/N: Y05504GL (GLOSS NASA BLUETONE

WHITE)

16. INSTALL HELICAL COIL INSERTS PER AEROSPACE INDUSTRIES

ASSOCIATION (AIA) SPECIFICATION NASM33537

17. INSTALL KEY-LOCK INSERTS (KEENSERTS) PER MILITARY

SPECIFICATION MS51835

18. INSTALL RIVETS PER AEROSPACE INDUSTRIES ASSOCIATION

(AIA) SPECIFICATION NASM47196

19. INSTALL BLIND RIVETS PER AEROSPACE INDUSTRIES

ASSOCIATION (AIA) SPECIFICATION NASM47195

20. PIN RIVET (HI-LOK) HOLE PREPARATION PER AEROSPACE

INDUSTRIES ASSOCIATION (AIA) SPECIFICATION NAS618 FOR

TRANSITIONAL FIT

21. PIN RIVET (HI-TIGUE) HOLE PREPARATION PER AEROSPACE

INDUSTRIES ASSOCIATION (AIA) SPECIFICATION NAS618 FOR

INTERFERENCE FIT

22. INSTALL HONEYCOMB INSERTS PER TPS 2-502, CAGE CODE

3GJB4

23. INSTALL CLICK BONDS PER DOCUMENT CBPS-206, CAGE CODE

66530. USE CLICK BOND CB200 ADHESIVE, CAGE CODE 66530

24 APPLY HUMAN-READABLE IDENTIFICATION MARKING PER MIL-

STD-130 BY <specify method LASER ENGRAVING, HANDWRITTEN, PERMANENT INK, DO NOT MARK. BAG AND TAG, or method optional>. USE 0.12 INCH CHARACTER HEIGHT.

LOCATE APPROXIMATELY AS

SHOWN. MARKING SHALL READ AS FOLLOWS:

"1JYR2 <- or ASSY> $PRPSHEET:{DwgNo}<dash number>"

SERIALIZE PER AFOP-7900.3-005

25 TIGHTEN ABOVE RUNNING TORQUE TO:

A. ### ± ###IN-LB

26 INSTALL SAFETY-WIRE AND/OR COTTER PINS PER AEROSPACE

INDUSTRIES ASSOCIATION (AIA) SPECIFICATION NASM33540

27. SEE AFRC DRAWING NO. <dwg number> FOR WIRING

INTERCONNECTION AND SPECIFIC ELECTRICAL COMPONENT

USAGE

28 OBTAIN FEATURES/DIMENSIONS NOT SHOWN/SURFACE PROFILE

FROM PART FILE <filename, revision>

29 APPLY HUMAN-READABLE IDENTIFICATION MARKING PER MIL-

STD-130 BY <specify method LASER ENGRAVING, HADNWRITTEN, PERMANENT INK, ADHESIVE LABEL, or optional method>. USE

0.12 INCH CHARACTER HEIGHT. LOCATE APPROXIMATELY AS

SHOWN. MARKING SHALL READ AS FOLLOWS: "SEE DRAWING

<dwg number> FOR MODIFICATION DOCUMENTATION"

30 BAG AND TAG IN ACCORDANCE WITH AFOP-7900.3-005.

HANDWRITTEN, PERMANENT INK OR OTHER HUMAN-READABLE

IDENTIFICATION TAG MARKING ACCEPTABLE. SERIALIZE PER

AFOP-7900.3-005

1. MATERIAL: MATERIAL: STEEL ASTM A572/A572M GRADE 50 OR

ASTM A992/A992M

2. PRIMER/TOP COAT FINISH PER MIL-DTL-18264 AS FOLLOWS:

A. ONE COAT MIL-PRF-23377 EPOXY PRIMER, TYPE I, CLASS

C1, C2, or N

B. TWO COATS MIL-PRF-85285 POLYURETHANE, TYPE II,

COLOR 15092 (OSHA SAFETY BLUE) PER SAE INTERNATIONAL

SPECIFICATION AMS-STD-595

C. MASK HOLES PRIOR TO PRIMER AND PAINT

3 APPLY HUMAN-READABLE IDENTIFICATION MARKING PER MIL-

STD-130 BY HANDWRITTEN, PERMANENT INK. USE 0.5 INCH

CHARACTER HEIGHT. LOCATE APPROXIMATELY AS

SHOWN. MARKING SHALL READ AS FOLLOWS:

"1JYR2-FLL-HPROJ-0011-APPROPRIATE DASH " AND LATEST

REVISION

4. INTERPRET DIMENSIONING AND TOLERANCING PER

ASME Y14.5-2018

5. UNLESS OTHERWISE SPECIFIED ALL SURFACES:

.063 A B

-101 STRONGBACK PLATE A DETAIL

SEE DETAIL A

3 FS

.125

DETAIL A

4 PLACES

SCALE 0.250

CONTROLLED BY: A.C. HOLGUIN, AFRC, NASA

CUI//SP-EXPT

REVIEWED FOR CUI BY: A.C. HOLGUIN, AFRC, NASA

(EXCEPT FOR EXPORT CONTROL)

The information contained in this document is technical in content, but not technical data as defined by the International Traffic in Arms Regulations (ITAR) or technology as defined by the Export Administration Regulations (EAR), and therefore is designated as EAR99/NLR, (No License Required). General Prohibition Six (Embargo) applies to all items subject to the EAR, (i.e. item on the CCL and within EAR99/NLR). You may not make an export or re-export contrary to the provisions of part 746 (Embargoes and Other Special Controls) of the EAR and 22 CFR §126.1 of the ITAR.

EAR99/NLR NOTICE

A B

Carla Masella Full Size

C

D

7 6 5 4 3

A

A

D

C

36X .812 +.010 -.001

THRU

5X .750-16 UNF-2B THRU

1.00

.000 12X .415

.000

12X 5.678

12X 6.508

7.884

2X 2.974

2X 3.053

14.937

X

X

X

X

X

X

X

X

X

X

X

X

135.820

6.000

4X R1.000

4X R1.000

SHEET 2 OF 9CI NO. SCALE: 0.125

-FLL-HPROJ-00111JYR2D

REV.DWG. NO.CAGESIZE

THREADED HOLE TABLE (ALL DIMS. BASIC)

Hole No. X Y

A1 0.000 0.000

A2 28.354 -0.052

A3 53.191 -0.067

A4 72.548 -0.012

A5 103.702 4.321

.032 A

.062 A B

Y

X

-103 STRONGBACK PLATE B DETAIL

MINOR DIA.

A1 A2 A3 A4

A5

.125

SEE DETAIL B

DETAIL B

2 PLACES

SCALE 0.250

CONTROLLED BY: A.C. HOLGUIN, AFRC, NASA

CUI//SP-EXPT

A

B

C

D

7 6 5 4 3

A

A

D

C

36X .812 +.010 -.001

THRU

2X .750-16 UNF-2B THRU

6X R1.000

6X .563-18 UNF-2B THRU

1.00

X

X

X

X

X

X

X

X

X

X

X

4.850

.000

12X 3.474 2X 1.850

12X 1.894

6.63712X 7.262

135.820

13.487

SHEET 3 OF 9CI NO. SCALE: 0.125

-FLL-HPROJ-00111JYR2D

REV.DWG. NO.CAGESIZE

THREADED HOLE TABLE (ALL DIMS. BASIC)

Hole No. X Y

A1 0.000 0.000

A2 19.676 -0.009

B1 -26.207 -6.038

B2 -23.090 -6.038

B3 40.927 2.131

B4 44.489 2.131

B5 40.927 -1.431

B6 44.489 -1.431

.032 A .019 1.25 A B

MINOR DIA.

.062 A B

-105 STRONGBACK PLATE C DETAIL

Y

X

MINOR DIA.

A1 A2

B1 B2

B3 B4

B5 B6

.125

CONTROLLED BY: A.C. HOLGUIN, AFRC, NASA

CUI//SP-EXPT

A

B

C

D

7 6 5 4 3

A

A

D

C

36X .812 +.010 -.001

THRU

.750-16 UNF-2B THRU

8X .625-18 UNF-2B THRU

6X R1.000

2X .563-18 UNF-2B THRU

1.00

4.500

4.000

4X R1.000

X

X

X

X

X

X

X

X

X

X

X

X

135.820

.000 12X 4.887

.000

6.263

12X 1.206

6X 5.876

12X 7.299

6.674 3.674

4.263

14.937

SHEET 4 OF 9CI NO. SCALE: 0.125

-FLL-HPROJ-00111JYR2D

REV.DWG. NO.CAGESIZE

THREADED HOLE TABLE (ALL DIMS. BASIC)

Hole No. X Y

A1 92.871 1.277

B1 -6.752 0.000

B2 -3.376 0.000

B3 0.000 0.000

B4 -6.752 -3.626

B5 0.000 -3.626

B6 -6.752 -7.252

B7 -3.376 -7.252

B8 0.000 -7.252

C1 23.426 4.980

C2 26.543 4.980

.037 .44 A

.019 1.25 A B .032 A B

.062 A B

-107 STRONGBACK PLATE D DETAIL

SEE DETAIL C

Y

X

SEE DETAIL D

MINOR DIA. MINOR DIA.

.125

DETAIL C

SCALE 0.250

Y

X

MINOR DIA.

A1

B1 B2 B3

B4 B5

B6 B7 B8

C1 C2

DETAIL D

6 PLACES

SCALE 0.250

CONTROLLED BY: A.C. HOLGUIN, AFRC, NASA

CUI//SP-EXPT

A B

C

D

7 6 5 4 3

A

A

D

C

36X .812 +.010 -.001

THRU

4X .563-18 UNF-2B THRU

4X .750-16 UNF-2B THRU

.000

5.184

.000

12X 3.808

12X 2.286

12X 8.379

3.184

4.754

1.184

X

X

X

X

X

X

X

X

X

X

X

X

X

X

14.937

6X R1.000

135.820

1.00

SHEET 5 OF 9CI NO. SCALE: 0.125

-FLL-HPROJ-00111JYR2D

REV.DWG. NO.CAGESIZE

THREADED HOLE TABLE (ALL DIMS. BASIC)

Hole No. X Y

A1 -61.178 -1.199

A2 -57.616 -1.199

A3 -61.178 -4.761

A4 -57.616 -4.761

B1 -34.749 -3.015

B2 -15.024 -2.968

B3 0.000 0.000

B4 -11.250 0.000

.032 A

.019 1.25 A B

MINOR DIA.

.062 A B

-109 STRONGBACK PLATE E DETAIL

Y

XA1 A2

A3 A4 B1 B2

B3B4

.125

CONTROLLED BY: A.C. HOLGUIN, AFRC, NASA

CUI//SP-EXPT

A

B

C

D

7 6 5 4 3

A

A

D

C

36X .812 +.010 -.001

THRU

3X .750-16 UNF-2B THRU

.000

10.230

.000

12X 8.855

12X 2.762

12X 3.332

2.708

14.937

X

X

X

X

X

X

X

X

X

X

X

X

9 6X R1.000

2X 2.230

1.00

SHEET 6 OF 9CI NO. SCALE: 0.125

-FLL-HPROJ-00111JYR2D

REV.DWG. NO.CAGESIZE

THREADED HOLE TABLE (ALL DIMS. BASIC)

Hole No. X Y

A1 -32.887 -0.471

A2 -13.205 -0.448

A3 0.000 0.000

.032 A

.062 A B

-111 STRONGBACK PLATE F DETAIL

Y

X

MINOR DIA.

A1 A2 A3

.125

CONTROLLED BY: A.C. HOLGUIN, AFRC, NASA

CUI//SP-EXPT

A

B

C

D

7 6 5 4 3

A

A

D

C

36X .812 +.010 -.001

THRU

4X R1.000

36X .812 +.010 -.001

THRU

8.000

8.000

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

X

12X .000

4X 4.094

12X .000

12X 6.093

12X 12.186

13.561

135.820

14.937

1.00

12X .000

12X 6.093

12X .000

12X 12.186

13.561

X

X

X

X

X

X

X

X

X

X

X

X

X

135.820

14.937

1.00

SHEET 7 OF 9CI NO. SCALE: 0.125

-FLL-HPROJ-00111JYR2D

REV.DWG. NO.CAGESIZE

.063 A

.063 A

-113 STRONGBACK PLATE G DETAIL

-115 STRONGBACK PLATE H DETAIL

SEE DETAIL E

3 FS

.125

DETAIL E

4 PLACES

SCALE 0.250

.125

CONTROLLED BY: A.C. HOLGUIN, AFRC, NASA

CUI//SP-EXPT

A B

B A

C

D

7 6 5 4 3

A

A

D

C

24X .812 +.010 -.001

THRU

60X .812 +.010 -.001

THRU

X

X

X

X

X

X

X

X

X

X

X

X

X

12X .000

12X 8.698

12X .000

10.074

135.820

11.450

1.00

12X .000

12X 6.812

12X .000

12X 13.624

12X 20.436

12X 27.248

28.624

30.000

1.00

X

X

X

X

X

X

X

X

X

X

X

X

X

135.820

SHEET 8 OF 9CI NO. SCALE: 0.125

-FLL-HPROJ-00111JYR2D

REV.DWG. NO.CAGESIZE

.063 A

.063 A

-117 STRONGBACK PLATE J DETAIL

-119 STRONGBACK PLATE K DETAIL

.125

.125

CONTROLLED BY: A.C. HOLGUIN, AFRC, NASA

CUI//SP-EXPT

A

B

A

B

C

D

7 6 5 4 3

A

A

D

C

48X .688 +.008 -.001

THRU

X

X

X

X

X

X

X

X

X

X

X

X

X

12X .000

12X 6.159

12X .000

12X 12.318

12X 18.477

20.104

135.820

21.480

1.00

SHEET 9 OF 9CI NO. SCALE: 0.125

-FLL-HPROJ-00111JYR2D

REV.DWG. NO.CAGESIZE

.063 A

-121 STRONGBACK PLATE L DETAIL

.125

CONTROLLED BY: A.C. HOLGUIN, AFRC, NASA

CUI//SP-EXPT

A

B